Agenda for this presentation is Exhaust options to reduce the launch numbers from 3 to 2: (1) Mass Reduction of Max-C Rover, ACO Orbiter, and or ACO ERS (2) Eliminate Max-C Rover (3) Launch vehicle options (4) Solar Sail for all interplanetary propulsion, chemical for maneuvering Goal would be to: (1) Brainstorm any other alternatives we have not considered (2) Eliminate any of the options listed above (3) Go forward with a possible viable option that is identified.


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    Title :

    DEPLOYTECH: Mars Sample Return Concept Study Delta Results


    Contributors:
    T. Russell (author)

    Publication date :

    2012


    Size :

    19 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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